Installation for fabricating a thermal protection covering of a body or of a rear assembly for a thruster, and associated methods

Patent metadata

Field	Value
Publication number	US-10843219-B2
Application number	US-201615337763-A
Country	US
Kind code	B2
Filing date	Oct 28, 2016
Priority date	Oct 30, 2015
Publication date	Nov 24, 2020
Grant date	Nov 24, 2020

Abstract

An installation for fabricating a thermal protection covering of a body or of a rear assembly for a thruster, includes an extruder presenting a die having an outlet orifice through which a strip of elastomer material is to be extruded, the extruder having a die control system to vary the size of the outlet orifice; a mandrel to be set into rotation about its axis; a deposition head to deposit the strip on the mandrel; a conveyor system to convey the strip from the outlet orifice of the die of the deposition head; and a thickness monitoring system to measure the thickness of the strip on the deposition head and on the mandrel and to compare each measured thickness value with a predetermined value, the thickness monitoring system to control the die control system so as to cause the size of the outlet orifice of the die to vary.

First claim

The invention claimed is:

1. An installation for fabricating a thermal protection covering of a body or of a rear assembly for a thruster, said installation comprising:
an extruder including a die having an outlet orifice through which a strip of elastomer material is to be extruded, the extruder being provided with a die control system configured to vary a size of the outlet orifice of the die;
a mandrel configured to be set into rotation about its axis;
a deposition head configured to deposit the strip of elastomer material on the mandrel, the deposition head and the mandrel being configured to be set into movement relative to each other along a longitudinal axis of the mandrel;
a conveyor system configured to convey the strip from the outlet orifice of the die to the deposition head; and
a thickness monitoring system configured to measure a first value of a thickness of the strip on the deposition head and configured to measure a second value of the thickness of the strip that has been deposited on the mandrel, the thickness monitoring system further including a processor to compare each of the first and second thickness values with a predetermined value to provide first and second comparison values, said thickness monitoring system also being configured, as a function of results of the comparisons of each of the first and second thickness values with the predetermined value that provide the first and second comparison values, to control the die control system so as to cause the size of the outlet orifice of the die to vary.

2. The installation according to claim 1 , further comprising a temperature monitoring system configured to measure a temperature of the strip on the deposition head and to compare a measured temperature value with a predetermined temperature value, the installation further comprising a first heater member configured to heat the strip in the die of the extruder, and a second heater member configured to heat the strip on the deposition head, the temperature monitoring system further being configured to act as a function of the result of the comparison between said measured temperature value and said predetermined temperature value to control at least one of the first and second heater members.

3. The installation according to claim 1 , wherein the deposition head comprises an applicator member for applying the strip on the mandrel, and the thickness monitoring system being further configured, as a function of the result of the thickness comparisons, to control an application pressure of the strip against the mandrel as imposed by the applicator member.

4. The installation according to claim 1 , wherein the deposition head comprises an applicator member for applying the strip on the mandrel and the installation further comprising a strip thickness adapter system for adapting the thickness of the strip and configured to control the die control system so as to increase the size of the outlet orifice following an increase in an application pressure of the strip against the mandrel as imposed by the applicator member.

5. The installation according to claim 1 , further comprising a speed adapter system configured to vary a speed at which the strip is deposited on the mandrel and to reduce, or respectively to increase, a speed of extrusion of the strip through the outlet orifice following a reduction, or respectively an increase, in the deposition speed of the strip on the mandrel.

6. The installation according to claim 1 , wherein the die is defined by at least two elements that co-operate with each other and that are movable relative to each other, the die control system being configured to move at least one of these elements so as to vary the size of the outlet orifice of the die.

Assignees

• Airbus Safran Launchers Sas
• Arianegroup Sas

Inventors

• Vennet Caroline
• Borie Edouard
• Rodolausse Julien
• Lassalle Pierre
• Munoz Matthieu
• Boirie Johan

Classifications

• B29C53/8041 Primary

  Measuring, controlling or regulating (B29C53/665 takes precedence) · CPC title

• B29C53/66

  with axially movable winding feed member {, e.g. lathe type winding} · CPC title

• B29L2031/3097

  Cosmonautical vehicles; Rockets · CPC title

• B29C48/151

  Coating hollow articles · CPC title

• B29C53/56

  Winding and joining, e.g. winding spirally {(winding in general B65H)} · CPC title